### 57786 Federal Register / Vol. 78, No. 183 / Friday, September 20, 2013 / Rules and Regulations

Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: (425) 227–1138; fax: (425) 227–1149. Information may be emailed to: 9–ANM–116– AMOC–REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(i) Related Information

Refer to Mandatory Continuing Airworthiness Information European Aviation Safety Agency Airworthiness Directive 2012–0182, dated September 11, 2012, for related information, which can be found in the AD docket on the Internet at http://www.regulations.gov.
(j) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(i) Airbus Mandatory Service Bulletin A330–92–3116, dated April 25, 2012

(ii) Reserved. (3) For service information identified in this AD, contact Airbus SAS—Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330–A340@airbus.com; Internet http://www.airbus.com.

(4) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221.

(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Renton, Washington on September 9, 2013. Jeffrey E. Duven, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2013–22542 Filed 9–19–13; 8:45 am]

**BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2013–0350; Directorate Identifier 2012–SW–050–AD; Amendment**  **39–17583; AD 2013–19–01]**

**RIN 2120–AA64**

**Airworthiness Directives; AgustaWestland S.p.A. Helicopters** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for AgustaWestland S.p.A. (AgustaWestland) Model A119 and AW119 MKII helicopters to require inspecting the pilot and co-pilot doors to ensure that the windows are properly bonded within the doors. If the windows are not properly bonded, the AD requires applying bonding to the windows, the seals, and the window frames of the pilot and co-pilot doors. This AD was prompted by the loss of a pilot-door window during a test flight. The actions of this AD are intended to ensure the windows do not detach from the doors, potentially injuring persons on the ground and damaging the helicopter’s tailboom and the tail rotor blades.

**DATES :**  This AD is effective October 25,
2013.

The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of October 25, 2013.

**ADDRESSES :**  For service information identified in this AD, contact AgustaWestland, Customer Support & Services, Via Per Tornavento 15, 21019 Somma Lombardo (VA) Italy, ATTN: Giovanni Cecchelli; telephone 39–0331– 711133; fax 39 0331 711180; or at http://www.agustawestland.com/technicalbullettins. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas
76137. Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov or in person at the Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the foreignauthority’s AD, any incorporated-byreference service information, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800–647–5527) is U.S. Department of Transportation, Docket Operations Office, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590.

**FOR FURTHER INFORMATION CONTACT :**  Sharon Miles, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222–5110; email sharon.y.miles@faa.gov.

**SUPPLEMENTARY INFORMATION :** 

Discussion

On April 25, 2013, at 78 FR 24367, the Federal Register published our notice of proposed rulemaking (NPRM), which proposed to amend 14 CFR part 39 to include an AD that would apply to AgustaWestland Model A119 and AW119 MKII helicopters, serial numbers up to and including 14781. The NPRM proposed to require inspecting the pilot and co-pilot doors to ensure that the windows are properly bonded within the doors. If the windows are not properly bonded, the NPRM proposed applying bonding to the windows, the seals, and the window frames of the pilot and co-pilot doors. The proposed requirements were intended to ensure the windows do not detach from the doors, potentially injuring persons on the ground and damaging the helicopter’s tailboom and the tail rotor blades.

The NPRM was prompted by EASA AD No. 2012–0058, dated April 3, 2012, issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. EASA issued AD No. 2012–0058 to correct an unsafe condition for AgustaWestland Model A119 and AW119 MKII helicopters. EASA advises that the pilot-door window detached during a test flight of an AW119 MKII helicopter. The occupant was not injured, and the helicopter was not damaged.

According to EASA, an investigation revealed that a ‘‘lack of the bonding of the seal both to the window and to the door structure’’ caused the window’s detachment. To address this unsafe condition, AugustaWestland issued Bollettino Tecnico (BT) 119–47, dated March 29, 2012, and EASA issued AD 2012–0058 to require an inspection of the bonding in the pilot and co-pilot door windows and, if there is no bonding, applying bonding.

If this condition is not corrected, it could lead to detachment of the


### 57787 Federal Register / Vol. 78, No. 183 / Friday, September 20, 2013 / Rules and Regulations

windows from the pilot- and co-pilot doors, potentially injuring persons on the ground and damaging the helicopter, EASA advises.

Comments

We gave the public the opportunity to participate in developing this AD, but we received no comments on the NPRM (78 FR 24367, April 25, 2013).

FAA’s Determination

These helicopters have been approved by the aviation authority of Italy and are approved for operation in the United States. Pursuant to our bilateral agreement with Italy, EASA, its technical representative, has notified us of the unsafe condition described in the EASA AD. We are issuing this AD because we evaluated all information provided by EASA and determined the unsafe condition exists and is likely to exist or develop on other helicopters of these same type designs and that air safety and the public interest require adopting the AD requirements as proposed.

Related Service Information

We reviewed BT 119–47 for all AgustaWestland A119 and AW119 MKII helicopters, which contains procedures to ensure that the pilot- and co-pilot door windows are correctly bonded. Costs of Compliance

We estimate that this AD affects 65 helicopters of U.S. Registry and that labor costs average $85 an hour. Based on these estimates, we expect the following costs:

• Inspecting for bonding between the seals and the windows in the internal and external sides of the junction areas requires a 0.5 work-hour for a labor cost of about $43. No parts are needed, so the cost for the U.S. fleet totals $2,795.

• Adding the bonding material if needed requires about 1.5 work-hours for a labor cost of about $128. The cost of materials is negligible. Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency’s authority.

We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ‘‘General requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on helicopters identified in this rulemaking action. Regulatory Findings

This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

(1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866;

(2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979);

(3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction; and

(4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

**PART 39—AIRWORTHINESS DIRECTIVES** 

■ 1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

**§ 39.13 [Amended]**

■ 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):
2013–19–01 AgustaWestland S.p.A.: Amendment 39–17583; Docket No. FAA–2013–0350; Directorate Identifier 2012–SW–050–AD.
(a) Applicability

This AD applies to AgustaWestland S.p.A. (AgustaWestland) Model A119 and AW119 MKII helicopters, serial numbers up to and including 14781, certificated in any category. (b) Unsafe Condition

This AD defines the unsafe condition as a window detaching from the pilot or co-pilot doors, which could result in damage to the helicopter and injury to persons on the ground.
(c) Effective Date

This AD becomes effective October 25,
2013. (d) Compliance

You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time.
(e) Required Actions

Within the next 50 hours time-in-service (TIS) or within the next five months, whichever comes first:

(1) Visually inspect the pilot and co-pilot doors by referencing Figure 1 of AugustaWestland Bollettino Tecnico 119–47, dated March 29, 2012 (BT), to determine whether there is bonding between the seal (3) and the window (4) in the internal and external side of the seal’s junction area.

(2) If there is no bonding, before further flight, apply bonding to the windows, seals, and window frames in accordance with the Compliance Instructions, paragraphs 5 through 20, of the BT.
(f) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Sharon Miles, Aviation Safety Engineer, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222– 5110; email sharon.y.miles@faa.gov.

(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC.
(g) Additional Information

The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2012–0058, dated April 3, 2012. You may view the EASA AD on the Internet at http:// www.regulations.gov in Docket No. FAA–
2013–0350. (h) Subject

Joint Aircraft Service Component (JASC) Code: 5610, Flight Compartment Windows.
(i) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) AgustaWestland Bollettino Tecnico 119–47, dated March 29, 2012.

(ii) Reserved.


### 57788 Federal Register / Vol. 78, No. 183 / Friday, September 20, 2013 / Rules and Regulations

(3) For AgustaWestland service information identified in this AD, contact AgustaWestland, Customer Support & Services, Via Per Tornavento 15, 21019 Somma Lombardo (VA) Italy, ATTN: Giovanni Cecchelli; telephone 39- 0331– 711133; fax 39 0331 711180; or at http://www.agustawestland.com/technicalbullettins.

(4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. For information on the availability of this material at the FAA, call (817) 222–5110.

(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Fort Worth, Texas, on September 9, 2013. Kim Smith, Directorate Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2013–22547 Filed 9–19–13; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 71**

**[Docket No. FAA–2013–0434; Airspace Docket No. 13–ANM–1]** 

**Amendment of Class E Airspace; Everett, WA** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  This action modifies Class E airspace at Everett, WA, to accommodate aircraft departing and arriving under Instrument Flight Rules (IFR) at Snohomish County Airport (Paine Field), WA. This action, initiated by the biennial review of the Snohomish County airspace area, enhances the safety and management of Instrument Flight Rules (IFR) operations at the airport. This action also adjusts the geographic coordinates of the airport.

**DATES :**  Effective date, 0901 UTC, December 12, 2013. The Director of the Federal Register approves this incorporation by reference action under 1 CFR Part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments.

**FOR FURTHER INFORMATION CONTACT :**  Eldon Taylor, Federal Aviation Administration, Operations Support Group, Western Service Center, 1601 Lind Avenue SW., Renton, WA, 98057; telephone (425) 203–4537.

**SUPPLEMENTARY INFORMATION :**  History

On July 10, 2013, the FAA published in the Federal Register a notice of proposed rulemaking (NPRM) to amend controlled airspace at Everett, WA (78 FR 41333). Interested parties were invited to participate in this rulemaking effort by submitting written comments on the proposal to the FAA. No comments were received.

Class E airspace designations are published in paragraph 6004, of FAA Order 7400.9X dated August 7, 2013, and effective September 15, 2013, which is incorporated by reference in 14 CFR 71.1. The Class E airspace designations listed in this document will be published subsequently in that Order.

The Rule

This action amends Title 14 Code of Federal Regulations (14 CFR) Part 71 by modifying Class E airspace designated as an extension to Class D surface area at Snohomish County Airport. To accommodate aircraft arriving and departing under instrument flight rules, a segment extends from the 4.5-mile radius of the airport to 8 miles northwest of the airport. This action, initiated by a biennial review of the airspace, enhances the safety and management of IFR operations at the airport. Also, the geographic coordinates of the airport are updated to coincide with the FAA’s aeronautical database.

The FAA has determined this regulation only involves an established body of technical regulations for which frequent and routine amendments are necessary to keep them operationally current. Therefore, this regulation: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034; February 26, 1979); and (3) does not warrant preparation of a regulatory evaluation as the anticipated impact is so minimal. Since this is a routine matter that only affects air traffic procedures and air navigation, it is certified this rule, when promulgated, does not have a significant economic impact on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. The FAA’s authority to issue rules regarding aviation safety is found in Title 49 of the U.S. Code. Subtitle 1, Section 106 discusses the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the agency’s authority. This rulemaking is promulgated under the authority described in Subtitle VII, Part A, Subpart I, Section 40103. Under that section, the FAA is charged with prescribing regulations to assign the use of airspace necessary to ensure the safety of aircraft and the efficient use of airspace. This regulation is within the scope of that authority as it modifies controlled airspace at Snohomish County Airport (Paine Field), Everett, WA.

Environmental Review

The FAA has determined that this action qualifies for categorical exclusion under the National Environmental Policy Act in accordance with FAA Order 1050.1E, ‘‘Environmental Impacts: Policies and Procedures,’’ paragraph 311a. This airspace action is not expected to cause any potentially significant environmental impacts, and no extraordinary circumstances exist that warrant preparation of an environmental assessment. List of Subjects in 14 CFR Part 71

Airspace, Incorporation by reference, Navigation (air). Adoption of the Amendment

In consideration of the foregoing, the Federal Aviation Administration amends 14 CFR Part 71 as follows:

**PART 71—DESIGNATION OF CLASS A, B, C, D AND E AIRSPACE AREAS; AIR**  **TRAFFIC SERVICE ROUTES; AND REPORTING POINTS** 

■ 1. The authority citation for 14 CFR Part 71 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40103, 40113, 40120; E. O. 10854, 24 FR 9565, 3 CFR, 1959– 1963 Comp., p. 389.

**§ 71.1 [Amended]**

■ 2. The incorporation by reference in 14 CFR 71.1 of the Federal Aviation Administration Order 7400.9X, Airspace Designations and Reporting Points, dated August 7, 2013, and effective September 15, 2013 is amended as follows:
Paragraph 6004 Class E Airspace Areas Designated as an Extension to Class D Surface Area
* * * * *

ANM WA E4 Everett, WA [Modified] Everett, Snohomish County Airport (Paine Field), WA (Lat. 47 ° 54 ′25 ′′ N, long. 122 ° 16′54′′ W) That airspace extending upward from the surface within 2.4 miles each side of the Snohomish County Airport (Paine Field) 341 ° bearing extending from the 4.5-mile radius of the airport to 8 miles northwest of the airport. This Class E airspace area is effective